Design optimization of non-axisymmetric endwall contouring in compressor cascade

被引：0
|
作者：
Zhao, Wei-Guang [1 ]
Jin, Dong-Hai [1 ]
Gui, Xing-Min [1 ]
机构：
[1] Beijing University of Aeronautics and Astronautics, Aeroengine Simulation Research Center, Beijing 100191, China
来源：
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics | 2013年 / 34卷 / 06期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Global optimization
引用
收藏
页码：1047 / 1050
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